EP1983203A3 - Device for rotating and clamping moveable flaps - Google Patents

Device for rotating and clamping moveable flaps Download PDF

Info

Publication number
EP1983203A3
EP1983203A3 EP20080007261 EP08007261A EP1983203A3 EP 1983203 A3 EP1983203 A3 EP 1983203A3 EP 20080007261 EP20080007261 EP 20080007261 EP 08007261 A EP08007261 A EP 08007261A EP 1983203 A3 EP1983203 A3 EP 1983203A3
Authority
EP
European Patent Office
Prior art keywords
flap
clamping
rotating
moveable flaps
rotation axis
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP20080007261
Other languages
German (de)
French (fr)
Other versions
EP1983203B1 (en
EP1983203A2 (en
Inventor
Helmut Thanhofer
Helmut Janker
Manfred Palik
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
EADS Deutschland GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Publication of EP1983203A2 publication Critical patent/EP1983203A2/en
Publication of EP1983203A3 publication Critical patent/EP1983203A3/en
Application granted granted Critical
Publication of EP1983203B1 publication Critical patent/EP1983203B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/08—Aerodynamic models
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F17/00—Special devices for shifting a plurality of wings operated simultaneously
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F15/00—Power-operated mechanisms for wings
    • E05F15/60—Power-operated mechanisms for wings using electrical actuators
    • E05F15/603—Power-operated mechanisms for wings using electrical actuators using rotary electromotors
    • E05F15/611—Power-operated mechanisms for wings using electrical actuators using rotary electromotors for swinging wings
    • E05F15/614—Power-operated mechanisms for wings using electrical actuators using rotary electromotors for swinging wings operated by meshing gear wheels, one of which being mounted at the wing pivot axis; operated by a motor acting directly on the wing pivot axis
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00—Application of doors, windows, wings or fittings thereof
    • E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
    • E05Y2900/502—Application of doors, windows, wings or fittings thereof for vehicles for aircraft or spacecraft

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Clamps And Clips (AREA)
  • Spinning Or Twisting Of Yarns (AREA)

Abstract

Die Erfindung betrifft eine Vorrichtung zum Drehen und Verklemmen einer bezüglich einer ersten Klappe (100) um eine Drehachse D beweglichen zweiten Klappe (200) umfassend eine Verdreheinrichtung (1a) und eine Klemmeinrichtung (1 b), wobei die Klemmeinrichtung (1 b) eine gegen die erste Klappe (100) und zweite Klappe (200) spannbare oder eine gegen die zweite Klappe (200) spannbare und sich gegen die erste Klappe (100) abstützende oder eine gegen die erste Klappe (100) spannbare und sich gegen die zweite Klappe (200) abstützende und in der Drehachse D angeordnete Spannhülse (3) aufweist und die Verdreheinrichtung (1a) eine an einer Klappe (100, 200) um die Drehachse D drehbar gelagerte antreibbare Welle (60) mit einem mit der anderen Klappe (200, 100) verbundenen Mitnehmer (50) oder Formschluss aufweist.

Figure imgaf001
The invention relates to a device for rotating and clamping a relative to a first flap (100) about a rotation axis D movable second flap (200) comprising a twisting device (1a) and a clamping device (1 b), wherein the clamping device (1 b) against the first flap (100) and the second flap (200) can be tensioned or stretched against the second flap (200) and supported against the first flap (100) or stretchable against the first flap (100) and against the second flap ( 200) supporting and arranged in the axis of rotation D clamping sleeve (3) and the twisting device (1a) on a flap (100, 200) rotatably mounted about the rotation axis D driven shaft (60) with one with the other flap (200, 100 ) connected carrier (50) or positive engagement.
Figure imgaf001
EP20080007261 2007-04-18 2008-04-12 Device for rotating and clamping moveable flaps Not-in-force EP1983203B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200710018189 DE102007018189B4 (en) 2007-04-18 2007-04-18 Device for twisting and clamping movable flaps

Publications (3)

Publication Number Publication Date
EP1983203A2 EP1983203A2 (en) 2008-10-22
EP1983203A3 true EP1983203A3 (en) 2012-08-01
EP1983203B1 EP1983203B1 (en) 2013-09-04

Family

ID=39619387

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20080007261 Not-in-force EP1983203B1 (en) 2007-04-18 2008-04-12 Device for rotating and clamping moveable flaps

Country Status (3)

Country Link
US (1) US7997539B2 (en)
EP (1) EP1983203B1 (en)
DE (1) DE102007018189B4 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005008331A1 (en) * 2005-02-23 2006-08-31 Airbus Deutschland Gmbh Shaft`s rotation angle determining device for use in aircraft, has motor detecting primary rotation data, and position pick up unit detecting secondary rotation data, where synchronization unit synchronizes both data
DE102010053277A1 (en) * 2010-12-02 2012-06-06 Airbus Operations Gmbh Locking fixture, recliner fixture, component system, main wing of an aircraft wind tunnel model and aircraft wind tunnel model with such a main wing
CN103807286B (en) * 2014-02-28 2016-08-17 仝达机电工业（惠州）有限公司 A kind of automatic turning device
US9643716B2 (en) * 2014-04-01 2017-05-09 The Boeing Company Air vehicle, actuator assembly and associated method of manufacture
CN113320715B (en) * 2021-07-07 2023-02-14 四川省天域航通科技有限公司 Wing strength test mechanism for unmanned aerial vehicle assembly
CN114735175A (en) * 2022-03-24 2022-07-12 西北工业大学 Wing rudder angle transformation structure of towing testing machine of underwater glider

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3731546A (en) * 1971-12-01 1973-05-08 Sundstrand Corp Power operable pivot joint
DE102004063774A1 (en) * 2004-12-30 2006-07-13 Schilling, Wolfgang Infinitely blockable hinge comprises expanding rubber ring between two metal discs with tensile bolt to expand and press against inside wall of upper hinge part

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2932473A (en) * 1957-03-26 1960-04-12 Martin Co Combined hinge, structural member and actuator for aircraft control surfaces
DE1283603B (en) * 1965-04-06 1968-11-21 Werner Altmann Locking device for two parts movable relative to one another about an axis of rotation
US4691582A (en) * 1984-01-30 1987-09-08 Weyer Paul P Thin profile rotary actuator with backlash elimination
DE3702294C1 (en) * 1987-01-27 1988-04-14 Messerschmitt Boelkow Blohm Actuator for wing flaps of aircraft
DE102005031990A1 (en) * 2005-07-08 2007-01-11 Stabilus Gmbh Device for motor- and power-operated moving a pivotable about a pivot axis flap of a vehicle
US7560888B2 (en) * 2005-09-08 2009-07-14 Honeywell International Inc. Electromechanical actuator including redundant, dissimilar position feedback
US7322545B2 (en) * 2005-12-29 2008-01-29 The Boeing Company Structural mechanism for unlocking and engaging a controllable surface on a hinged platform (wing)

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3731546A (en) * 1971-12-01 1973-05-08 Sundstrand Corp Power operable pivot joint
DE102004063774A1 (en) * 2004-12-30 2006-07-13 Schilling, Wolfgang Infinitely blockable hinge comprises expanding rubber ring between two metal discs with tensile bolt to expand and press against inside wall of upper hinge part

Also Published As

Publication number Publication date
EP1983203B1 (en) 2013-09-04
DE102007018189A1 (en) 2008-10-30
US7997539B2 (en) 2011-08-16
DE102007018189B4 (en) 2010-06-17
US20080258015A1 (en) 2008-10-23
EP1983203A2 (en) 2008-10-22

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